STARLINK-34060, 63815
Orbit data source: Space-Track
STARLINK-34060, 63815 is a payload satellite owned by SpaceX/Seattle (US) in LEO that was launched on Sun, 04 May 2025 UTC via an FALCON 9 launch vehicle from the Air Force Eastern Test Range (AFETR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
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63815 intel report (Beta)
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Identifier
Orbit
Country
USRelated business
Manufacturer
SpaceX/Seattle
Mission
Operational Commercial Communications
Bus & Motor
STARLINK V2MO, Unknown motor
Mass
575 kg wet, ~530 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 17.7 m
Radar Cross Section
41.120 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 12 hours ago
TLE from 12 hours ago
0 STARLINK-34060
1 63815U 25092M 26315.10389969 .00018595 00000-0 68332-3 0 9996
2 63815 42.9962 220.6563 0001605 258.3334 101.7338 15.27590923 86247Epoch: 2026-11-11T02:29Z
TLE epoch observation values (Epoch: 2026-11-11T02:29:36.933Z)
Latitude
0.00003°
Longitude
132.9959°
Altitude
483.015 km
Speed
7.626 km/s
True Right ascension
14h 42m 37s
True Declination
0° 00' 00"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
11:05:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
486.064 km
Perigee altitude
483.861 km
Semi-major axis
6,863.099 km
Eccentricity
0.00016
Inclination
42.9962°
RAAN
220.6563°
Arg. of periapsis
258.3334°
True anomaly
101.75181°
Mean anomaly
101.7338°
Eccentric anomaly
101.7428°
Mean motion
3.81736 °/min
Orbital period
94.31 mins
BSTAR
0.00068332
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Other satellites on launch #92 in the year 2025 (2025-05-04 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.STARLINK-34060 Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-11-11 21:33:30.668Z | 228.433° WSW | 2026-11-11 21:35:30.668Z | 185.635° SSW | 52.99° | 2026-11-11 21:39:30.668Z | 76.515° E |
| 6 mins | 2026-11-11 23:12:30.668Z | 278.537° WNW | 2026-11-11 23:14:30.668Z | 322.785° NNW | 52.434° | 2026-11-11 23:18:30.668Z | 71.289° E |
| 6 mins | 2026-11-12 00:51:30.668Z | 293.159° NW | 2026-11-12 00:54:30.668Z | 39.817° NE | 56.41° | 2026-11-12 00:57:30.668Z | 90.156° ESE |
| 6 mins | 2026-11-12 02:30:30.668Z | 275.837° WNW | 2026-11-12 02:33:30.668Z | 183.392° SSW | 44.992° | 2026-11-12 02:36:30.668Z | 133.284° SE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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